Global Patent Index - EP 2571762 A1

EP 2571762 A1 20130327 - TILT WING AIRCRAFT

Title (en)

TILT WING AIRCRAFT

Title (de)

KIPPFLÜGEL-FLUGZEUG

Title (fr)

AÉRONEF À AILES BASCULANTES

Publication

EP 2571762 A1 20130327 (DE)

Application

EP 11720497 A 20110519

Priority

  • DE 102010021022 A 20100519
  • EP 2011058141 W 20110519

Abstract (en)

[origin: CA2798023A1] The invention relates to a tilt wing aircraft having a rear drive/control unit which is designed to generate propulsion and to generate an upward or downward directed propulsion component and/or a laterally directed propulsion component even in the hovering and in the climb mode of the aircraft.

IPC 8 full level

B64C 29/00 (2006.01); B64C 27/82 (2006.01); B64D 27/24 (2006.01)

CPC (source: EP US)

B64C 27/22 (2013.01 - US); B64C 29/0033 (2013.01 - EP US); B64D 27/24 (2013.01 - EP US); B64C 2027/8236 (2013.01 - EP US); B64C 2201/042 (2013.01 - EP US); B64C 2201/108 (2013.01 - EP US); B64D 2027/026 (2013.01 - EP US); Y02T 50/60 (2013.01 - EP US); Y10S 903/902 (2013.01 - US)

Citation (search report)

See references of WO 2011144696A1

Designated contracting state (EPC)

AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

DOCDB simple family (publication)

DE 102010021022 A1 20111124; BR 112012029118 A2 20180515; CA 2798023 A1 20111124; EP 2571762 A1 20130327; EP 2571762 B1 20141203; ES 2531843 T3 20150320; US 2013099065 A1 20130425; WO 2011144696 A1 20111124

DOCDB simple family (application)

DE 102010021022 A 20100519; BR 112012029118 A 20110519; CA 2798023 A 20110519; EP 11720497 A 20110519; EP 2011058141 W 20110519; ES 11720497 T 20110519; US 201213675646 A 20121113